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CN107093794B - Array antenna for generating dual-mode vortex electromagnetic field - Google Patents

Array antenna for generating dual-mode vortex electromagnetic field Download PDF

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CN107093794B
CN107093794B CN201710299588.9A CN201710299588A CN107093794B CN 107093794 B CN107093794 B CN 107093794B CN 201710299588 A CN201710299588 A CN 201710299588A CN 107093794 B CN107093794 B CN 107093794B
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CN107093794A (en
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朱诚
徐鹏
黄琪
贾晋晓
郭翀
梁昌洪
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Xian University of Electronic Science and Technology
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    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01QANTENNAS, i.e. RADIO AERIALS
    • H01Q1/00Details of, or arrangements associated with, antennas
    • H01Q1/36Structural form of radiating elements, e.g. cone, spiral, umbrella; Particular materials used therewith
    • H01Q1/38Structural form of radiating elements, e.g. cone, spiral, umbrella; Particular materials used therewith formed by a conductive layer on an insulating support
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01QANTENNAS, i.e. RADIO AERIALS
    • H01Q1/00Details of, or arrangements associated with, antennas
    • H01Q1/50Structural association of antennas with earthing switches, lead-in devices or lightning protectors
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01QANTENNAS, i.e. RADIO AERIALS
    • H01Q21/00Antenna arrays or systems
    • H01Q21/0006Particular feeding systems
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01QANTENNAS, i.e. RADIO AERIALS
    • H01Q21/00Antenna arrays or systems
    • H01Q21/29Combinations of different interacting antenna units for giving a desired directional characteristic

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Abstract

本发明公开了一种用于产生双模态涡旋电磁场的阵列天线,主要解决现有技术产生涡旋电磁场模态单一,阵列口径利用率低的问题。其包括8个阵列单元(T)、馈电网络(K)、介质基板(J)、同轴探针(D)和金属地板(G),8个阵列单元(T)和馈电网络(K)均印制在介质基板(J)的上表面,金属地板(G)印制在介质基板(J)的下表面;馈电网络(K)设有一个输入端口和8个输出端口,该输入端与同轴探针(D)连接,以实现同轴探针(D)对馈电网络(K)的馈电;该8个输出端口依次与8个阵列单元(T)对应连接,以实现馈电网络(K)对阵列单元(T)的馈电。本发明能产生两种模态的涡旋电磁波,可用于无线通信系统前端。

The invention discloses an array antenna for generating a dual-mode vortex electromagnetic field, which mainly solves the problems in the prior art that the mode of the vortex electromagnetic field is single and the utilization rate of the array aperture is low. It includes 8 array units (T), feed network (K), dielectric substrate (J), coaxial probe (D) and metal floor (G), 8 array units (T) and feed network (K ) are printed on the upper surface of the dielectric substrate (J), and the metal floor (G) is printed on the lower surface of the dielectric substrate (J); the feed network (K) has an input port and 8 output ports, the input The end is connected to the coaxial probe (D) to realize the feeding of the coaxial probe (D) to the feed network (K); the 8 output ports are connected to the 8 array units (T) in sequence to realize The feed network (K) feeds the array unit (T). The invention can generate vortex electromagnetic waves in two modes, and can be used in the front end of a wireless communication system.

Description

用于产生双模态涡旋电磁场的阵列天线Array antenna for generating dual-mode vortex electromagnetic fields

技术领域technical field

本发明属于天线技术领域,具体涉及一种用于产生双模态涡旋电磁场的阵列天线,可用于无线通信系统,卫星通信系统和雷达探测。The invention belongs to the technical field of antennas, in particular to an array antenna for generating dual-mode vortex electromagnetic fields, which can be used in wireless communication systems, satellite communication systems and radar detection.

背景技术Background technique

涡旋电磁波是有别于普通平面波的一类电磁波,平面波只有自旋角动量,而涡旋电磁波不仅具有自旋角动量,还有轨道角动量,它的等相位面由于波束携带轨道角动量而呈螺旋状分布,其与平面波的等相位平面是不同的。涡旋电磁波可以有不同的模态数l,不同的l代表不同的涡旋程度,理论上来讲l有无限多个取值,并且不同模态之间是相互正交的。这一特性为提高频谱利用率和信道容量提供了一个理想的发展方向。Vortex electromagnetic waves are a type of electromagnetic waves different from ordinary plane waves. Plane waves only have spin angular momentum, while vortex electromagnetic waves not only have spin angular momentum, but also orbital angular momentum. It is distributed in a helical shape, which is different from the equiphase plane of the plane wave. Vortex electromagnetic waves can have different mode numbers l, and different l represents different degrees of vortex. In theory, l has infinitely many values, and different modes are orthogonal to each other. This feature provides an ideal development direction for improving spectrum utilization and channel capacity.

通过对国内外研究现状的跟踪可以看出,目前国内外学者提出一些产生涡旋电磁场的方法,例如文献“Q.Bai,A.Tennant and B.Allen.Experimental circular phasedarray for generating OAM radio beams[J].Electronics Letters,25th September2014,Vol.50No.20:pp.1414–1415.”中公开的基于微带阵列天线产生单模态涡旋电磁场的方法,其将8个阵列单元等间隔分布在同心圆上,各阵列单元依次与馈电网络各输出端口相连接,组成的圆形阵列天线,以产生单一模态的涡旋电磁场。这种方法组成的阵列天线虽然增益较高,且剖面低,易于共形,但该阵列天线只能产生单一模态的涡旋电磁场,无法同时对多个模态进行复用,阵列孔径利用率较低。Through the tracking of the research status at home and abroad, it can be seen that scholars at home and abroad have proposed some methods of generating vortex electromagnetic fields, such as the literature "Q. Bai, A. Tennant and B. Allen. Experimental circular phased array for generating OAM radio beams [J ].Electronics Letters,25th September2014,Vol.50No.20:pp.1414–1415.”The method disclosed in the microstrip array antenna to generate a single-mode vortex electromagnetic field, which distributes 8 array elements at equal intervals concentrically On the circle, each array unit is sequentially connected to each output port of the feed network to form a circular array antenna to generate a single-mode vortex electromagnetic field. Although the array antenna formed by this method has high gain, low cross-section, and is easy to be conformal, the array antenna can only generate a single-mode vortex electromagnetic field, and cannot multiplex multiple modes at the same time. lower.

发明内容Contents of the invention

本发明的目的在于针对上述现有技术的不足,提出一种用于产生双模态涡旋电磁场的阵列天线,以增加生成涡旋电磁场的模态数量,提高阵列天线的口径利用率。The object of the present invention is to address the shortcomings of the above-mentioned prior art and propose an array antenna for generating a dual-mode vortex electromagnetic field, so as to increase the number of modes for generating a vortex electromagnetic field and improve the aperture utilization of the array antenna.

为实现上述目的,本发明用于产生双模态涡旋电磁场的阵列天线,包括8个阵列单元、馈电网络、介质基板、同轴探针和金属地板,8个阵列单元和馈电网络均印制在介质基板的上表面,金属地板印制在介质基板的下表面,其特征在于:In order to achieve the above object, the present invention is used to generate the array antenna of dual-mode vortex electromagnetic field, including 8 array units, feed network, dielectric substrate, coaxial probe and metal floor, and 8 array units and feed network are all Printed on the upper surface of the dielectric substrate, the metal floor is printed on the lower surface of the dielectric substrate, characterized in that:

每个阵列单元均为H形贴片,每个H形贴片的一端表面开有U形槽,以使每个阵列单元工作在0.9GHz和1.8GHz这两个频点;Each array unit is an H-shaped patch, and one end of each H-shaped patch has a U-shaped groove on the surface, so that each array unit works at two frequency points of 0.9GHz and 1.8GHz;

馈电网络中设有两组双枝节阻抗匹配器,以使馈电网络工作在0.9GHz和1.8GHz;There are two sets of dual stub impedance matchers in the feed network to make the feed network work at 0.9GHz and 1.8GHz;

馈电网络中还设有8个差相馈电枝节,以在各相邻阵列单元之间实现差相馈电,即在0.9GHz的频点,这8个差相馈电枝节依次实现各相邻阵列单元之间的相位相差45°,在1.8GHz的频点,这8个差相馈电枝节依次实现各相邻阵列单元之间的相位相差90°。There are also 8 differential-phase feed branches in the feed network to realize differential-phase feed between adjacent array units, that is, at the frequency point of 0.9GHz, these 8 differential-phase feed branches realize each phase in turn. The phase difference between the adjacent array units is 45°, and at the frequency point of 1.8 GHz, these eight phase-differential feed branches sequentially realize the phase difference between each adjacent array unit by 90°.

上述阵列天线,其特征在于:馈电网络设有一个输入端口和8个输出端口,该输入端与同轴探针连接,以实现同轴探针对馈电网络的馈电;该8个输出端口依次与8个阵列单元对应连接,以实现馈电网络对阵列单元的馈电。The above-mentioned array antenna is characterized in that: the feed network is provided with an input port and 8 output ports, and the input port is connected with the coaxial probe to realize the feeding of the coaxial probe to the feed network; the 8 output ports The ports are correspondingly connected to the 8 array units in turn, so as to realize the power feeding of the array units by the feed network.

上述阵列天线,其特征在于:两组双枝节阻抗匹配器均为2节级联的阶梯形阻抗匹配器,各节长度均为λ0.9/6,其中,λ0.9为0.9GHz对应的工作波长。The above-mentioned array antenna is characterized in that: the two sets of dual stub impedance matchers are 2 cascaded ladder-shaped impedance matchers, and the length of each section is λ 0.9 /6, wherein λ 0.9 is the corresponding working wavelength of 0.9GHz.

上述阵列天线,其特征在于:两组双枝节阻抗匹配器于同轴探针所在位置上下,左右对称。The above-mentioned array antenna is characterized in that: two sets of double-twig impedance matchers are located up and down at the position of the coaxial probe, and are symmetrical left and right.

上述阵列天线,其特征在于:第一过渡枝节和第二过渡枝节于同轴探针所在位置上下,左右对称。The above-mentioned array antenna is characterized in that: the first transition branch and the second transition branch are up and down at the position of the coaxial probe, and left and right symmetrical.

上述阵列天线,其特征在于:其特征在于8个差相馈电枝节均为蛇形结构的微带传输线,其中,第一差相馈电枝节与第五差相馈电枝节,第二差相馈电枝节与第六差相馈电枝节,第三差相馈电枝节与第七差相馈电枝节,第四差相馈电枝节与第八差相馈电枝节这四对差相馈电枝节均于同轴探针所在位置上下对称。The above-mentioned array antenna is characterized in that: it is characterized in that the eight differential-phase feeding branches are microstrip transmission lines with a serpentine structure, wherein, the first differential-phase feeding branch and the fifth differential-phase feeding branch, and the second differential-phase feeding branch The four pairs of differential phase feeders are the feeder branch and the sixth differential phase feeder branch, the third differential phase feeder branch and the seventh differential phase feeder branch, the fourth differential phase feeder branch and the eighth differential phase feeder branch The branches are symmetrical up and down at the position of the coaxial probe.

上述阵列天线,其特征在于:每个差相馈电枝节的拐角外设有斜切率为p的切线,该切线与拐角外侧的距离为L1,且切线与馈线底边之间的夹角为45°,拐角内侧与拐角外侧之间的距离为L2,斜切率p=L1/L2The above-mentioned array antenna is characterized in that: a tangent line with an inclination rate p is set outside the corner of each differential feed branch, the distance between the tangent line and the outside of the corner is L 1 , and the angle between the tangent line and the bottom edge of the feed line is is 45°, the distance between the inside of the corner and the outside of the corner is L 2 , and the bevel ratio p=L 1 /L 2 .

上述阵列天线,其特征在于:第一组双枝节阻抗匹配器设有2个,第一过渡枝节设有2个,第二过渡枝节设有4个,第二组双枝节阻抗匹配器设有4个,每2个过渡枝节4连接组成一对。The above-mentioned array antenna is characterized in that: the first group of dual stub impedance matchers is provided with 2, the first transition stub is provided with 2, the second transition stub is provided with 4, and the second group of dual stub impedance matchers is provided with 4 , and every 2 transition branches are connected to form a pair.

上述阵列天线,其特征在于:所述第一组的2个双枝节阻抗匹配器,其每个的第一枝节与每个第一过渡枝节对应连接,其每个第二枝节与每对第二过渡枝节对应连接,即2个第二枝节分别与两对过渡枝节对应连接;所述第二组的每个双枝节阻抗匹配器,其每个第一枝节与每个第二过渡枝节对应连接,其每个第二枝节与每对差相馈电枝节对应连接,即4个第二枝节分别与四对差相馈电枝节对应连接。The above-mentioned array antenna is characterized in that: the first group of 2 dual-stub impedance matchers, each of the first stubs is connected to each first transition stub, and each second stub is connected to each pair of the first transition stubs. The two transition branches are correspondingly connected, that is, the two second branches are respectively connected to the two pairs of transition branches; each of the two-branch impedance matchers of the second group corresponds to each of the first branches and each of the second transition branches Each of the second branches is connected to each pair of differential-phase feeding branches, that is, the four second branches are respectively connected to four pairs of differential-phase feeding branches.

上述阵列天线,其特征在于:所述8个阵列单元的尺寸完全相同,且等间隔地分布在半径为R圆周上,其中,R取值为1.8GHz对应的波长。The above-mentioned array antenna is characterized in that: the dimensions of the eight array elements are exactly the same, and they are distributed at equal intervals on a circle with a radius R, wherein R is a wavelength corresponding to 1.8 GHz.

与现有技术相比,本发明具有如下优点:Compared with prior art, the present invention has following advantage:

1.本发明在同一阵列口径下能产生双模涡旋电磁场,可实现对涡旋电磁场的多种模态进行复用,提高了阵列天线的口径利用率。1. The present invention can generate a dual-mode vortex electromagnetic field under the same array aperture, which can realize the multiplexing of multiple modes of the vortex electromagnetic field, and improves the aperture utilization rate of the array antenna.

2.本发明可在0.9GHz和1.8GHz这两个频点工作,增加了工作频率带宽。2. The present invention can work at two frequency points of 0.9GHz and 1.8GHz, increasing the working frequency bandwidth.

3.本发明采用H型微带天线作为天线阵列单元,有效减小了阵列单元尺寸,使组成的阵列天线的结构更加紧凑。3. The present invention adopts the H-shaped microstrip antenna as the antenna array unit, which effectively reduces the size of the array unit and makes the structure of the formed array antenna more compact.

附图说明Description of drawings

图1为本发明实施例的结构示意图;Fig. 1 is the structural representation of the embodiment of the present invention;

图2为本发明实施例的回波损耗曲线图;Fig. 2 is the return loss curve figure of the embodiment of the present invention;

图3为本发明实施例在0.9GHz的涡旋电磁波束模态值为1的远场辐射方向图;3 is a far-field radiation pattern with a vortex electromagnetic beam mode value of 1 at 0.9 GHz according to an embodiment of the present invention;

图4为本发明实施例在1.8GHz的涡旋电磁波束模态值为2的远场辐射方向图;4 is a far-field radiation pattern with a vortex electromagnetic beam mode value of 2 at 1.8 GHz according to an embodiment of the present invention;

图5为本发明实施例在0.9GHz的涡旋电磁波束模态值为1的近场电场分布图;FIG. 5 is a near-field electric field distribution diagram of a vortex electromagnetic beam with a modal value of 1 at 0.9 GHz according to an embodiment of the present invention;

图6为本发明实施例在1.8GHz的涡旋电磁波束模态值为2的近场电场分布图。FIG. 6 is a near-field electric field distribution diagram of a vortex electromagnetic beam with a mode value of 2 at 1.8 GHz according to an embodiment of the present invention.

具体实施方式Detailed ways

下面结合附图对本发明的实施例作进一步的详细说明:Embodiments of the present invention are described in further detail below in conjunction with accompanying drawings:

参照图1,本发明主要由8个阵列单元T、馈电网络K、介质基板J、同轴探针D和金属地板G组成,8个阵列单元T、馈电网络K均印制在介质基板J的上表面,金属地板G印制在介质基板J的下表面,同轴探针D依次穿过金属地板G和介质基板J,并与馈电网络K的输入端口相连接,其中:Referring to Fig. 1, the present invention is mainly composed of 8 array units T, feed network K, dielectric substrate J, coaxial probe D and metal floor G, and the 8 array units T and feed network K are all printed on the dielectric substrate On the upper surface of J, the metal floor G is printed on the lower surface of the dielectric substrate J, and the coaxial probe D passes through the metal floor G and the dielectric substrate J in turn, and is connected to the input port of the feeding network K, where:

所述金属地板G采用铜板。The metal floor G adopts copper plate.

所述介质基板J,采用环氧树脂,此种材料的介电常数为4.2,介质基板J的厚度为5mm,长度和宽度均为500mm。The dielectric substrate J is made of epoxy resin, the dielectric constant of this material is 4.2, the thickness of the dielectric substrate J is 5mm, and the length and width are both 500mm.

所述阵列单元T,均采用H形贴片,每个单元的长L0=70mm,宽W0=74mm;在每个单元两侧的中心位置开有第一矩形槽,在每个单元底边的中心位置开有第二矩形槽,在每个单元的一端开有U型槽。The array unit T adopts H-shaped patches, each unit has a length of L 0 =70 mm and a width of W 0 =74 mm; a first rectangular slot is opened at the center of both sides of each unit, and at the bottom of each unit A second rectangular slot is opened at the center of the side, and a U-shaped slot is opened at one end of each unit.

所述馈电网络K,包括第一组双枝节阻抗匹配器2,3、第二组双枝节阻抗匹配器5,6、第一过渡枝节1、第二过渡枝节4和8个差相馈电枝节7,8,9,10,11,12,13,14,其中,差相馈电枝节7,8构成第一对差相馈电枝节,差相馈电枝节9,10构成第二对差相馈电枝节,差相馈电枝节11,12构成第三对差相馈电枝节,差相馈电枝节13,14构成第四对差相馈电枝节;第一组双枝节阻抗匹配器2,3设有2个,第二组双枝节阻抗匹配器5,6设有4个,第一过渡枝节1设有2个,第二过渡枝节4设有4个,每2个第二过渡枝节4连接组成一对;The feed network K includes a first set of dual stub impedance matchers 2, 3, a second set of dual stub impedance matchers 5, 6, a first transition stub 1, a second transition stub 4, and 8 differential phase feeders Branches 7, 8, 9, 10, 11, 12, 13, 14, among them, the differential phase feeding branches 7 and 8 constitute the first pair of differential phase feeding branches, and the differential phase feeding branches 9 and 10 constitute the second pair of differential Phase feed branches, differential phase feed branches 11, 12 constitute the third pair of differential phase feed branches, and differential phase feed branches 13, 14 constitute the fourth pair of differential phase feed branches; the first group of double branch impedance matchers 2 , 3 is provided with 2, the second group of dual-branch impedance matching devices 5, 6 is provided with 4, the first transition branch 1 is provided with 2, the second transition branch 4 is provided with 4, and every 2 second transition branches 4 connected to form a pair;

该第一组双枝节阻抗匹配器2,3和第二组双枝节阻抗匹配器5,6均采用2节级联的阶梯形阻抗匹配器,且第一组双枝节阻抗匹配器2,3和第二组双枝节阻抗匹配器5,6于同轴探针D所在位置上下,左右对称;该第一过渡枝节1和第二过渡枝节4均采为矩形结构的微带传输线,且第一过渡枝节1和第二过渡枝节4于同轴探针D所在位置上下,左右对称;该8个差相馈电枝节7,8,9,10,11,12,13,14均为蛇形结构的微带传输线,其中,第一差相馈电枝节7与第五差相馈电枝节11,第二差相馈电枝节8与第六差相馈电枝节12,第三差相馈电枝节9与第七差相馈电枝节13,第四差相馈电枝节10与第八差相馈电枝节14这四对差相馈电枝节均于同轴探针D所在位置上下对称;每个差相馈电枝节的拐角外设有斜切率为p的切线,其中,切线与拐角外侧的距离为L1且与馈线底边之间的夹角为45°,拐角内侧与拐角外侧之间的距离为L2,斜切率p=L1/L2。这些部件的连接关系如下:The first group of dual-stub impedance matchers 2, 3 and the second group of dual-stub impedance matchers 5, 6 all use 2 cascaded ladder-shaped impedance matchers, and the first group of dual-stub impedance matchers 2, 3 and The second group of double-twig impedance matchers 5, 6 are symmetrical up and down at the position of the coaxial probe D; the first transition branch 1 and the second transition branch 4 are all adopted as microstrip transmission lines with a rectangular structure, and the first transition The branch 1 and the second transition branch 4 are symmetrical up and down at the position of the coaxial probe D; the eight differential phase feeding branches 7, 8, 9, 10, 11, 12, 13, and 14 are all serpentine structures Microstrip transmission line, wherein, the first differential phase feeding branch 7 and the fifth differential phase feeding branch 11, the second differential phase feeding branch 8 and the sixth differential phase feeding branch 12, the third differential phase feeding branch 9 The four pairs of differential phase feeding branches 13, the fourth differential phase feeding branch 10 and the eighth differential phase feeding branch 14 are symmetrical up and down at the position of the coaxial probe D; The corner of the phase feed branch is provided with a tangent line with a bevel rate p, wherein the distance between the tangent line and the outside of the corner is L 1 and the angle between the bottom edge of the feeder line is 45°, and the distance between the inside of the corner and the outside of the corner is The distance is L 2 , and the inclination rate p=L 1 /L 2 . The connections of these components are as follows:

第一组双枝节阻抗匹配器2,3,其每个第一枝节2与每个第一过渡枝节1对应连接,其每个第二枝节3与每对第二过渡枝节4对应连接,即2个第二枝节3分别与两对第二过渡枝节4对应连接;In the first group of dual-stub impedance matching devices 2, 3, each of the first stubs 2 is correspondingly connected to each of the first transition stubs 1, and each of its second stubs 3 is correspondingly connected to each pair of second transition stubs 4, namely The two second branches 3 are correspondingly connected with two pairs of second transition branches 4;

第二组双枝节阻抗匹配器5,6,其每个第一枝节5与每个第二过渡枝节4对应连接,其每个第二枝节6与每对差相馈电枝节对应连接,即两个差相馈电枝节是一端连接组成一对差相馈电枝节,并于连接处与第二枝节6末端的中心位置连接,以实现每个第二枝节6与每对差相馈电枝节对应连接,进而得到4个第二枝节6分别与第一对差相馈电枝节7,8、第二对差相馈电枝节9,10、第三对差相馈电枝节11,12、第四对差相馈电枝节13,14对应连接;The second group of dual-stub impedance matchers 5, 6, each of its first stubs 5 is correspondingly connected to each of the second transition stubs 4, and each of its second stubs 6 is correspondingly connected to each pair of differential phase feeding stubs, that is Two differential-phase feeding branches are connected at one end to form a pair of differential-phase feeding branches, and are connected to the center of the end of the second branch 6 at the connection, so as to realize the connection between each second branch 6 and each pair of differential-phase feeding branches. Corresponding connection, and then four second branches 6 are respectively connected with the first pair of differential phase feeding branches 7, 8, the second pair of differential phase feeding branches 9, 10, the third pair of differential phase feeding branches 11, 12, the third pair of differential phase feeding branches Four pairs of differential-phase feeding stubs 13 and 14 are connected correspondingly;

为保证馈电网络K的8个输出端口的输出阻抗与阵列单元T的输入阻抗相匹配,需将馈电网络K的每个差相馈电枝节分别深入到每个阵列单元T的第二矩形槽内部,并与第二矩形槽顶边中心位置连接;8个阵列单元T依次与馈电网络K的8个输出端口对应连接,8个阵列单元T等间距分布在半径R=166mm的圆周上。In order to ensure that the output impedance of the eight output ports of the feed network K matches the input impedance of the array unit T, each differential phase feed branch of the feed network K needs to be deep into the second rectangle of each array unit T The inside of the slot is connected to the center of the top edge of the second rectangular slot; the 8 array units T are connected to the 8 output ports of the feed network K in turn, and the 8 array units T are equally spaced on the circumference of the radius R=166mm .

上述H形贴片开设的槽参数、馈电网络K的双枝节阻抗匹配器参数、过渡枝节的参数,及差相馈电枝节的斜切率和输出端口的宽度,均根据微带天线理论进行优化设置,本实施例采用但不局限于取如下参数:The slot parameters of the above-mentioned H-shaped patch, the parameters of the double-stub impedance matching device of the feed network K, the parameters of the transition stubs, and the skew rate of the differential-phase feed stubs and the width of the output port are all calculated according to the microstrip antenna theory. For optimization settings, this embodiment adopts, but is not limited to, the following parameters:

第一矩形槽长度d=35mm,宽度s=10.5mm;第二矩形槽长度Lm=31.5mm,宽度Wm=6.85mm;U型槽长度Ls=16mm,宽度Ws=3mm,其中,U型槽距单元边缘距离df=1mm;馈电网络K的8个端口宽度均为Wf=4.85mm;The first rectangular groove length d=35mm, width s=10.5mm; second rectangular groove length L m =31.5mm, width W m =6.85mm; U-shaped groove length L s =16mm, width W s =3mm, wherein, The distance between the U-shaped groove and the edge of the unit is df = 1mm; the width of the 8 ports of the feed network K is W f = 4.85mm;

两组双枝节阻抗匹配器2,3的宽度分别为6mm和12.6mm,长度分别为40.3mm和13mm;过渡枝节1和4的宽度均为9mm,长度分别为10mm以及17mm;8个差相馈电枝节7,8,9,10,11,12,13,14的斜切率分别为p1=0.92,p2=0.95,p3=0.85,p4=0.85,p5=0.92,p6=0.95,p7=0.85,p8=0.85。The widths of two sets of double stub impedance matchers 2 and 3 are 6mm and 12.6mm, and the lengths are 40.3mm and 13mm respectively; the widths of transition stubs 1 and 4 are both 9mm, and the lengths are 10mm and 17mm respectively; 8 differential phase feed The oblique cutting ratios of electrical branches 7, 8, 9, 10, 11, 12, 13, and 14 are p1=0.92, p2=0.95, p3=0.85, p4=0.85, p5=0.92, p6=0.95, p7=0.85 , p8=0.85.

本实施例中,通过馈电网络K对8个阵列单元T等幅差相馈电,相邻阵列单元T之间相位差为其中N=8,l为涡旋电磁波束的模态值,且需满足0<l<N/2。通过调节差相馈电枝节7,8,9,10,11,12,13,14的长度,从而实现相邻阵列单元T之间合理的相位差 In this embodiment, 8 array units T are fed with equal amplitude and phase difference through the feed network K, and the phase difference between adjacent array units T is Where N=8, l is the modal value of the vortex electromagnetic beam, and must satisfy 0<l<N/2. A reasonable phase difference between adjacent array units T can be achieved by adjusting the lengths of the differential phase feed branches 7, 8, 9, 10, 11, 12, 13, and 14

在0.9GHz,阵列天线上半部分的4个差相馈电枝节7,8,9,10的长度依次增加λ0.9/8,其中,λ0.9为0.9GHz对应的工作波长,从而实现这4个差相馈电枝节7,8,9,10的输出相位差为45°;由于阵列天线上半部分与其下半部分关于同轴探针D所在位置对称,因此阵列天线下半部分4个差相馈电枝节11,12,13,14的输出相位差,与其上半部分4个差相馈电枝节7,8,9,10的输出相位差相同,即阵列天线下半部分的4个差相馈电枝节11,12,13,14的输出相位差也为45°;根据镜像原理,第五个差相馈电枝节11的输出相位与第一个差相馈电枝节7的输出相位相差为180°,第六个差相馈电枝节12的输出相位与第二个差相馈电枝节8的输出相位相差为180°,第七个差相馈电枝节13的输出相位与第三个差相馈电枝节9的输出相位相差为180°,第八个差相馈电枝节14的输出相位与第四个差相馈电枝节10的输出相位相差为180°。At 0.9GHz, the lengths of the four phase-differential feed stubs 7, 8, 9, and 10 in the upper part of the array antenna increase in turn by λ 0.9 /8, where λ 0.9 is the working wavelength corresponding to 0.9GHz, so as to realize the four The output phase difference of phase-differential feeding stubs 7, 8, 9, and 10 is 45°; since the upper half of the array antenna and its lower half are symmetrical about the location of the coaxial probe D, the four phase difference phases of the lower half of the array antenna The output phase difference of the feed branches 11, 12, 13, 14 is the same as the output phase difference of the 4 different-phase feed branches 7, 8, 9, 10 in the upper half, that is, the 4 phase-differences of the lower half of the array antenna The output phase difference of feed branches 11, 12, 13, and 14 is also 45°; according to the mirror image principle, the output phase difference between the output phase of the fifth differential-phase feed branch 11 and the output phase difference of the first differential-phase feed branch 7 is 180°, the output phase difference of the sixth phase-differential feeding branch 12 and the output phase of the second differential-phase feeding branch 8 is 180°, the output phase of the seventh differential-phase feeding branch 13 is different from the third The phase difference between the output phases of the phase feed branch 9 is 180°, and the output phase difference between the eighth phase difference feed branch 14 and the output phase of the fourth phase difference feed branch 10 is 180°.

综上,实现8个差相馈电枝节7,8,9,10,11,12,13,14的输出相位差均为由于8个差相馈电枝节7,8,9,10,11,12,13,14分别与8个阵列单元T相连接,最终在0.9GHz实现相邻阵列单元T之间的相位差 In summary, the output phase differences of the 8 differential phase feed branches 7, 8, 9, 10, 11, 12, 13, and 14 are all Since the 8 phase difference feed branches 7, 8, 9, 10, 11, 12, 13, and 14 are respectively connected to 8 array units T, the phase difference between adjacent array units T is finally realized at 0.9GHz

根据微带传输线理论,当阵列天线工作频率由0.9GHz变为1.8GHz时,这8个差相馈电枝节7,8,9,10,11,12,13,14之间的相位差变为90°,最终实现在1.8GHz相邻阵列单元T之间的相位差 According to the microstrip transmission line theory, when the operating frequency of the array antenna is changed from 0.9GHz to 1.8GHz, the phase difference between the eight differential phase feeding stubs 7, 8, 9, 10, 11, 12, 13, and 14 becomes 90°, finally realize the phase difference between adjacent array elements T at 1.8GHz

本实施例中,在0.9GHz,相邻阵列单元T之间的相位差可以获得模态值l=1的涡旋电磁波束;在1.8GHz,各阵列单元T之间的相位差可以获得模态值l=2的涡旋电磁波束。In this embodiment, at 0.9GHz, the phase difference between adjacent array units T A vortex electromagnetic beam with mode value l=1 can be obtained; at 1.8GHz, the phase difference between each array unit T A vortex electromagnetic beam with mode value l=2 can be obtained.

本实施例的效果可通过以下仿真进一步说明:The effect of this embodiment can be further illustrated by the following simulation:

一.仿真条件:采用电磁仿真软件HFSS15.0对上述阵列天线模型进行仿真。1. Simulation conditions: use the electromagnetic simulation software HFSS15.0 to simulate the above array antenna model.

二.仿真内容:2. Simulation content:

仿真1,对本发明实施例的回波损耗进行仿真,其仿真结果如图2所示,由图2的回波损耗曲线图可见,本发明的阵列天线在0.9GHz和1.8GHz的回波损耗均小于-25dB,阵列天线的工作状态良好。Simulation 1, the return loss of the embodiment of the present invention is simulated, and its simulation result is as shown in Figure 2, as can be seen from the return loss curve diagram of Figure 2, the return loss of the array antenna of the present invention is both at 0.9GHz and 1.8GHz If it is less than -25dB, the working condition of the array antenna is good.

仿真2,对本发明实施例在0.9GHz的远场辐射方向图进行仿真,其仿真结果如图3所示,由图3的远场辐射方向图可以看出,远场辐射方向图在阵列天线正上方形成能量凹陷,这符合涡旋电磁波的特性。Simulation 2 is to simulate the far-field radiation pattern of the embodiment of the present invention at 0.9 GHz, and the simulation result is shown in Figure 3, as can be seen from the far-field radiation pattern of Figure 3, the far-field radiation pattern is in the front of the array antenna An energy depression is formed above, which conforms to the characteristics of vortex electromagnetic waves.

仿真3,对本发明实施例在1.8GHz的远场辐射方向图进行仿真,其仿真结果如图4所示,由图4的远场辐射方向图可以看出,远场辐射方向图在阵列天线正上方形成能量凹陷,符合涡旋电磁波的特性。Simulation 3 is to simulate the far-field radiation pattern of the embodiment of the present invention at 1.8 GHz. The simulation result is shown in FIG. 4. As can be seen from the far-field radiation pattern of FIG. An energy depression is formed above, which conforms to the characteristics of vortex electromagnetic waves.

仿真4,对本发明实施例在0.9GHz的近场电场分布图进行仿真,其仿真结果如图5所示,由图5的近场电场分布图可以看出,当涡旋电磁场模态值为1时,近场电场分布为2条顺时针旋转的轨道曲线。Simulation 4 is to simulate the near-field electric field distribution diagram of the embodiment of the present invention at 0.9 GHz. The simulation results are shown in Figure 5. As can be seen from the near-field electric field distribution diagram in Figure 5, when the vortex electromagnetic field modal value is 1 , the near-field electric field distribution is two orbital curves rotating clockwise.

仿真5,对本发明实施例在1.8GHz的近场电场分布图进行仿真,其仿真结果如图6所示,由图6的近场电场分布图可以看出,当涡旋电磁场模态值为2时,近场电场分布为4条顺时针旋转的轨道曲线。Simulation 5 is to simulate the near-field electric field distribution diagram of the embodiment of the present invention at 1.8 GHz. The simulation results are shown in Figure 6. As can be seen from the near-field electric field distribution diagram in Figure 6, when the vortex electromagnetic field modal value is 2 , the near-field electric field distribution is four orbital curves rotating clockwise.

由仿真4与仿真5可见,近场电场分布为多条顺时针的轨道曲线,这与不同模态值的轨道角动量波束特性一致,表明本发明的阵列天线可以产生涡旋电磁波特性良好的电磁波。It can be seen from simulation 4 and simulation 5 that the near-field electric field is distributed as a plurality of clockwise orbital curves, which is consistent with the beam characteristics of orbital angular momentum of different modal values, indicating that the array antenna of the present invention can produce electromagnetic waves with good vortex electromagnetic wave characteristics .

Claims (8)

1. a kind of for generating the array antenna of bimodal vortex electromagnetic field, including 8 array elements (T), feeding network (K), Medium substrate (J), coaxial probe (D) and metal floor (G), 8 array elements (T) and feeding network (K) are printed on medium The upper surface of substrate (J), metal floor (G) are printed on the lower surface of medium substrate (J), it is characterised in that:
Each array element (T) is H-shaped patch, the first rectangular channel is provided in the center of each unit two sides, each The center on unit bottom edge is provided with the second rectangular channel, is provided with U-type groove in one end of each unit, so that each array element work Make in the two frequency points of 0.9GHz and 1.8GHz;
It is equipped with two groups of double minor matters impedance matching boxs in feeding network (K), respectively first group double minor matters impedance matching box (2,3), With second group of double minor matters impedance matching box (5,6) so that feeding network work is in 0.9GHz and 1.8GHz;
8 differences mutually feed minor matters (7,8,9,10,11,12,13,14) is additionally provided in feeding network (K), in each adjacent array list Realize that difference is mutually fed between first (T), the turning of each difference mutually feed minor matters is externally provided with the tangent line that beveling rate is p, the tangent line with turn Distance on the outside of angle is L1, and the angle between tangent line and feeder line bottom edge is 45 °, on the inside of turning and the distance between on the outside of turning For L2, beveling rate p=L1/L2, i.e., in the frequency point of 0.9GHz, mutually feed minor matters successively realize each adjacent array element to this 8 differences (T) 45 ° of the phase phase difference between, in the frequency point of 1.8GHz, mutually feed minor matters successively realize each adjacent array element to this 8 differences (T) 90 ° of the phase phase difference between;8 differences mutually feed the micro-strip that minor matters (7,8,9,10,11,12,13,14) are serpentine configuration Transmission line.
2. array antenna according to claim 1, it is characterised in that: feeding network (K) is equipped with an input port and 8 Output port, the input terminal are connect with coaxial probe (D), to realize coaxial probe (D) to the feed of feeding network (K);This 8 Output port is successively correspondingly connected with 8 array elements (T), to realize feeding network (K) to the feed of array element (T).
3. array antenna according to claim 1, it is characterised in that: two groups of double minor matters impedance matching boxs are 2 assistant wardens connection Stairstepping impedance matching box, each length that saves is λ0.9/ 6, wherein λ0.9For the corresponding operation wavelength of 0.9GHz.
4. array antenna according to claim 1, it is characterised in that: two groups of double minor matters impedance matching boxs are in coaxial probe (D) above and below position, bilateral symmetry.
5. array antenna according to claim 1, it is characterised in that: First Transition minor matters (1) and the second transition minor matters (4) Above and below the position coaxial probe (D), bilateral symmetry.
6. array antenna according to claim 1, it is characterised in that: first group of double minor matters impedance matching box (2,3) is equipped with 2 A, First Transition minor matters (1) are equipped with 2, and the second transition minor matters (4) are equipped with 4, second group of double minor matters impedance matching box (5,6) Equipped with 4, every 2 transition minor matters (4) connection partners.
7. array antenna according to claim 6, it is characterised in that:
The double minor matters impedance matching boxs (2,3) of 2 of described first group, the first minor matters (2) of each of which and each First Transition branch Section (1) is correspondingly connected with, each of which second minor matters (3) is correspondingly connected with each pair of second transition minor matters (4), i.e. 2 the second minor matters (3) It is correspondingly connected with respectively with two pairs of transition minor matters (4);
Each of described second group double minor matters impedance matching box (5,6), each of which first minor matters (5) and each second transition minor matters (4) it is correspondingly connected with, mutually feed minor matters are correspondingly connected with each of which second minor matters (6) with each pair of difference, i.e. 4 the second minor matters (6) are respectively With first pair of difference mutually feed minor matters (7,8), second pair of difference mutually feed minor matters (9,10), third to poor mutually feed minor matters (11,12), Mutually mutually feed minor matters are correspondingly connected with this four pairs differences of feed minor matters (13,14) 4th pair of difference.
8. array antenna according to claim 1, it is characterised in that: the complete phase of size of 8 array elements (T) Together, it and is equally spaced in radius as on R circumference, wherein R value is the corresponding wavelength of 1.8GHz.
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